Boeing 747-123

Service difficulty reports · 2,292

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '747123'
  ORDER BY difficulty_date DESC"

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SDR UPS05443970Floorbeam · corrodedINSPECTION TYPE: C, BS 460 RBL 66 - 65 FLOORBEAM WEB CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 4 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM WEB REPAIR AS PER SRM 53-10-07 FIG 11.Feb 12, 2005 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443969Floorbeam · corrodedINSPECTION TYPE: C, BS 460, RBL 11 - 30 FLOORBEAM WEB CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 3 EXCEED SRM 53-10-01 FIG 1, LIMIT FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11.Feb 12, 2005 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443960Cargo Track · corrodedINSPECTION TYPE: C, BS 480 - 500 LBL 84 TIE DOWN TRACK I/B FLANGE & LIP FOUND CORRODED. CORROSION BLEND OUT 0.047 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Feb 12, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443950Cargo Track · corrodedINSPECTION TYPE: C, BS 440 - 460 LBL 86 TIE DOWN TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.044 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Feb 12, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443940Cargo Track · corrodedINSPECTION TYPE: C, BS 160 - 180 RBL 13 TIE DOWN TRACK I/B FLANGE & LIP FOUND CORRODED. CORROSION BLEND OUT 0.040 X .5 X 3 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01 PG 1.Feb 12, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443939Seat Track · corrodedINSPECTION TYPE: C, BS 190 - 240 RBL 11 - 33 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.046 X 1 X 5 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9.Feb 12, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0501321Smoke · detectedCREW REPORTED WHEN POWER WAS REDUCED FOR DESCENT. SMOKE WAS SEEN COMING FROM AIR CONDITIONING SYSTEM. GRADUALLY REDUCED TO NOTHING OVER 15 MINUTES TIME. INSPECTED AIR CONDITIONING SYSTEM AND ACM’S. PERFORMED OPERATION CK PER 21-20-00. NO DEFECTS NOTED. OFeb 12, 2005 · N858FT · Boeing 747123 · Cabin Cooling SystemSDR UPS05443941Cargo Track · crackedINSPECTION TYPE:C M/D- BS 355 - 360, RBL 72, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK (CRACK LENGTH 1 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Feb 11, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443926Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 6 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 11, 2005 · N676UP · Boeing 747123 · Wing SparSDR UPS05443925Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 8 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 11, 2005 · N676UP · Boeing 747123 · Wing SparSDR UPS05443924Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 NR 4 HOLE FOUND CRACKED AT INTERNAL SPLICE FITTING APPROX 0.060 INCH. HOLE REWORK PER SB 747-57A2314.Feb 11, 2005 · N676UP · Boeing 747123 · Wing SparSDR UPS05443990Skin · crackedINSPECTION TYPE: C, BS 1306 BETWEEN S24-25R R3 DOOR SKIN FOUND CRACK (CRACK LENGTH 1.25 INCH). M/D BS 1306 BETWEEN STR 24R-25R DOOR 3R SKIN REPAIRED PER SRM 52-00-03 FIG 4.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS05443989Cargo Track · crackedINSPECTION TYPE: C, TIE DOWN TRACK BEAM LWR CHORD BS1000-1002 LBL 33 CORROSION CRACK FOUND. CRACK LENGTH 1 INCH AND CORROSION BLEND OUT 0.060 X 1 X 3 INCH, EXCEED SRM 53-10-01 LIMIT. M/D TIE DOWN TRACK BEAM LOWER CHORD REPAIRED AS PER HX RS R53-45-35264 & ENFeb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443987Fitting · corrodedINSPECTION TYPE:C M/D BS 1580 LBL 80 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 INCH, EXCEED SRM 53-10-01 LIMIT. FITTING REPLACED PER SRM 51-10-01.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443986Fitting · corrodedINSPECTION TYPE: C, BS 1560, RBL 18 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.020 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1. LIMIT FITTING REPLACED PER SRM 51-10-01.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443985Cargo Track · corrodedINSPECTION TYPE: C, BS 1500, RBL 78 TIE DOWN SUPPORT FITTING CORROSION FOUND. CORROSION BLEND OUT 0.025 X 1 X 1 EXCEED SRM 53-10-01 LIMIT. FITTING REPLACED PER SRM 51-10-01.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443982Intercostal · corrodedINSPECTION TYPE: C, INTERCOSTAL BS 1420, LBL 11-33 HEAVY CORRODED. CORROSION BLEND OUT 0.060 X 1 X 1. EXCEED SRM 53-10-01 LIMIT. INTERCOSTAL REPAIRED AS PER SRM 51-40-04 FIG 1.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443981Intercostal · crackedINSPECTION TYPE: C, INTERCOSTAL BS 1300, LBL 11-33 RT O/B END CRACKED AT LWR SURFACE (CRACK LENGTH .75 INCH). INTERCOSTAL REPAIRED AS PER SRM 51-40-04 FIG 1.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443972Support Fitting · crackedINSPECTION TYPE: C, TIE DOWN TRACK / BS 1000 B/H VERTICAL SUPPORT FTG CRACKED AT LBL 33 (CRACK LENGTH 1 INCH). M/DECK TIE DOWN TRACK BS 1000 B/H VERTICAL SUPPORT FTG REPLACED AT LBL 33 AREA AS PER SRM 51-10-01 PG 9.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443965Seat Track · corrodedINSPECTION TYPE: C, BS 1500 - 1560, LBL 98 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 1480-1570 LBL 98 AREA.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443962Seat Track · corrodedINSPECTION TYPE:C, BS 1580-1600 LBL 33 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.045 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPLACED AT BS 1480 TO BS 1600 LBL 33 AS PER SRM 51-10-01 PG 9.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443961Cargo Track · corrodedINSPECTION TYPE: C, BS 1480 - 1500 RBL 34, TIE DOWN TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443959Seat Track · corrodedINSPECTION TYPE:C M/D- BS 1600 - 1640 RBL 98 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.040 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. SEAT TRACK REPAIR AS PER SRM 53-10-05 FIG 1A.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443957Seat Track · crackedINSPECTION TYPE:C M/D- BS 1580 TO 1600 LBL 98 SEAT TRACK CRACKED (CRACK LENGTH 1 INCH). SEAT TRACK REPAIRED FROM BS 1570 TO BS 1630 LBL 98 AS PER SRM 53-10-05 FIG 1A.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443952Floor Support · corrodedINSPECTION TYPE: C, STA 1330, LBL 65 FLOOR SUPPORT SURFACE CORROSION. CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443949Channel · corrodedINSPECTION TYPE: C, BS 1440, RBL 80-99 FLOOR SUPPORT U-CHANNEL ANCHOR NUTS AREA UPPER AND LOWER FACE FOUND CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT U-CHANNEL REPLACED AS PER SRM 51-10-01 PG 9.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443948Channel · corrodedINSPECTION TYPE: C, BS 1294, RBL 55-75 FLOOR SUPPORT U-CHANNEL UPPER FACE CORROSION FOUND CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT U-CHANNEL REPLACED AS PER SRM 51-10-01 PG 9.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443928Floorbeam · corrodedINSPECTION TYPE: C, M/D BS 1500 RBL 5-10 FLOORBEAM FOUND CORROSION. CORROSION BLEND OUT 2 X 2 X 0.060 INCH FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1.Feb 10, 2005 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443923Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 5 FOUND CRACKED .125 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123 · Wing SparSDR UPS05443922Skin · crackedINSPECTION TYPE:C, RHW REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND CRACKED AT HOLE NR 7 AT SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123 · Wing, Plate/SkinSDR UPS05443921Skin · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 FOUND HOLE NR 12 CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123 · Wing, Plate/SkinSDR UPS05443920Skin · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.Feb 10, 2005 · N676UP · Boeing 747123 · Wing, Plate/SkinSDR UPS05443964Seat Track · corrodedINSPECTION TYPE: C, SEAT TRACK BS 1497 - 1500 LBL 33 RT FLANGE CORRODED. CORROSION BLEND OUT 0.030 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1. TIE DOWN TRACK REPLACED AT BS 1480 TO BS 1600 LBL 33 AS PER SRM 51-10-01 PG 9.Feb 9, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443958Cargo Track · corrodedINSPECTION TYPE: C, BS 1660, RBL 78 TIE DOWN TRACK I/B FLANGE LWR FACE FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. TIE DOWN TRACK REPAIR AS PER SRM 53-10-05 FIG 1A.Feb 9, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443956Floor Support · crackedINSPECTION TYPE: C, STN 1094-1100 LBL 75 LONGITUDINAL FLOOR SUPPORT WEB & LOWER CHORD FOUND CRACKED (CRACK LENGTH 3.5 INCH). SUPPORT WEB REPLACED PER SRM 51-10-01 PG 9. LOWER CHORD REPAIRED PER HAECO RS R53-45-35260 & UPS ENG'R FILE 747-53-20227.Feb 9, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443946Floorbeam · corrodedINSPECTION TYPE:C - STA 1500, LBL 65 FLOORBEAM UPPER SURFACE CORROSION. CORROSION BLEND OUT 0.050 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1.Feb 9, 2005 · N676UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS05443919Skin · crackedINSPECTION TYPE: C, LT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.060 INCH. HOLE REWORKED AT BSB 747-57A2314.Feb 9, 2005 · N676UP · Boeing 747123 · Wing, Plate/SkinSDR P5CA0501317Actuator · malfunctionedINBOUND CREW REPORTED RUDDER RATIO LIGHT ON STEADY. T/S FOUND LOWER RUDDER ACTUATOR STUCK IN HIGH SPEED MODE. REMOVED AND REPLACED LOWER RUDDER RATIO ACTUATOR AND CONTROLLER PER MM 27-21-12. ALL OPS NORMAL.Feb 9, 2005 · N858FT · Boeing 747123 · Rudder ActuatorSDR UPS05444005Support Fitting · crackedINSPECTION TYPE:C M/D BS 1000 RBL 11 SEAT TRACK END SUPPORT FITTING FOUND CRACKED. SUPPORT FITTING REPLACED PER SRM 51-10-01 PG 9.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443974Seat Track · corrodedINSPECTION TYPE: C, BS 1165, RBL 75 SEAT TRACK FLANGE CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1, LIMIT SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443973Seat Track · crackedINSPECTION TYPE: C, BS 994 TO BS 995 RBL 98 SEAT TRACK CRACKED (CRACK LENGTH 1 INCH). M/ DECK BS 970 TO BS 995 RBL 98 TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443966Seat Track · crackedINSPECTION TYPE: C, BS 1140 - 1160, RBL 34 TIE DOWN TRACK FLANGE FOUND CRACKED (CRACK LENGTH 2.75 INCH). BS 1070 TO BS 1210 RBL 34 INCH TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 34.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443963Seat Track · crackedINSPECTION TYPE: C, BS 996 TO 999 RBL 75 SEAT TRACK CRACKED (CRACK LENGTH 1.5 INCH). TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A AT BS 930 TO BS 1000 RBL 75 AREA.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443953Attach Bracket · corrodedINSPECTION TYPE: C, BS 1020, RBL 75 FLOOR SUPPORT ATTACH BRACKET CORROSION FOUND. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PG 9.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS05443951Floor Support · corrodedINSPECTION TYPE: C, BS 1300, LBL 11- RBL 11, FLOOR SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.035 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS05443947Seat Track · corrodedINSPECTION TYPE: C, BS 1110 RBL 75 SEAT TRACK WEB ATTACH STIFFENER FOUND CORRODED. CORROSION BLEND OUT 0.020 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1, LIMIT. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05443930Bulkhead · crackedINSPECTION TYPE: C, BS 1480 BULKHEAD APU DUCT CUTOUT FOUND 3 FASTENER HOLES CRACKED. BS 1480 BULKHEAD REPAIRED PER SB 747-53-2309 UPS EO B747-5310-3100-C & DWG 144U2602.Feb 8, 2005 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS05443931Web · crackedINSPECTION TYPE: C, NR 2 PYLON REAR LOWER WEB AT NAC STN 212 I/B EDGE UPPER SURFACE RIVETS HOLES FOUND CRACKED. NAC STN 212 REAR LOWER WEB REPAIRED PER SRM 54-10-03 FIG 2.Feb 7, 2005 · N676UP · Boeing 747123 · Nacelle/Pylon, Main FrameSDR UPS05444006Rib · crackedINSPECTION TYPE:C RIGHT WING ILES 1057.55, 21 V/C FLAP I/B ARM O/B RIB FWD VERTICAL MOUNTING ATTACH FASTENER HOLES CRACKED (CRACK LENGTH 1 INCH). RIGHT WING 21 VC FLAP I/B ARM O/B RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R-57-41-35262 AND UPS EO B747-574Feb 5, 2005 · N676UP · Boeing 747123 · Wing, Rib/BulkheadSDR UPS05443997Rib · crackedINSPECTION TYPE:C RIGHT WING 17 VC FLAP O/B ARM O/B RIB MOST FWD FASTENER HOLE CRACKED (CRACK LENGTH 1.25 INCH). RIGHT WING 17 VC FLAP O/B ARM O/B RIB FWD FLANGE FASTENER HOLES REPAIRED AS PER HX RS R57-41-35263 AND UPS EO B747-5740-21796-A.Feb 5, 2005 · N676UP · Boeing 747123 · Wing, Rib/Bulkhead
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